SU1326188A3 - Method of forming servo motor body member and joining it with rigidity part - Google Patents
Method of forming servo motor body member and joining it with rigidity part Download PDFInfo
- Publication number
- SU1326188A3 SU1326188A3 SU823390752A SU3390752A SU1326188A3 SU 1326188 A3 SU1326188 A3 SU 1326188A3 SU 823390752 A SU823390752 A SU 823390752A SU 3390752 A SU3390752 A SU 3390752A SU 1326188 A3 SU1326188 A3 SU 1326188A3
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- base
- stiffness
- ring
- ring part
- flat
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims description 11
- 230000002093 peripheral effect Effects 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 claims description 3
- 238000007493 shaping process Methods 0.000 claims 1
- 239000003351 stiffener Substances 0.000 claims 1
- 238000004642 transportation engineering Methods 0.000 abstract 1
- 230000003993 interaction Effects 0.000 description 2
- 241001547021 Thecopus Species 0.000 description 1
- 230000008034 disappearance Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
- B23P19/10—Aligning parts to be fitted together
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
- B60T13/00—Transmitting braking action from initiating means to ultimate brake actuator with power assistance or drive; Brake systems incorporating such transmitting means, e.g. air-pressure brake systems
- B60T13/10—Transmitting braking action from initiating means to ultimate brake actuator with power assistance or drive; Brake systems incorporating such transmitting means, e.g. air-pressure brake systems with fluid assistance, drive, or release
- B60T13/24—Transmitting braking action from initiating means to ultimate brake actuator with power assistance or drive; Brake systems incorporating such transmitting means, e.g. air-pressure brake systems with fluid assistance, drive, or release the fluid being gaseous
- B60T13/46—Vacuum systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/26—Making other particular articles wheels or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
- B60T17/00—Component parts, details, or accessories of power brake systems not covered by groups B60T8/00, B60T13/00 or B60T15/00, or presenting other characteristic features
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49861—Sizing mating parts during final positional association
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Braking Systems And Boosters (AREA)
- Making Paper Articles (AREA)
- Motor Or Generator Frames (AREA)
- Hydraulic Turbines (AREA)
- Manufacture Of Motors, Generators (AREA)
- Prostheses (AREA)
- Braking Arrangements (AREA)
Abstract
Изобретение относитс к транспортному машиностроению. Цель изобретени - повьш ение надежности корпуса . Обечайка 2 опираетс на кольцевую станину 8, а к детали 5, помещенной на внутреннюю поверхность 6 основани 3, прикладывают усилие определенной величины по стрелке А с помощью толкател 9 в форме диска. 4 3.п. ф-лы, 3 ил. СОFIELD: transport engineering. The purpose of the invention is to increase the reliability of the case. The shell 2 rests on the ring base 8, and a detail of 5 placed on the inner surface 6 of the base 3 is applied by a certain amount of force along arrow A with the help of the pusher 9 in the form of a disk. 4 3.p. f-ly, 3 ill. WITH
Description
1 one
Изобретение относитс к автомобильным тормозным устройствам, .в частности к сервомоторам вакуумного типа.This invention relates to automobile braking devices, in particular vacuum-type servomotors.
Цель изобретени - повьшение надежности корпуса.The purpose of the invention is to increase the reliability of the housing.
На фиг. изображен элемент корпуса , установленный на кольцевой станине, разрез; на фиг.2 - то же, вариант; на фиг.З - то же, после снти прикладываемого усили .FIG. shows a housing element mounted on a ring frame, a section; figure 2 - the same option; on fig.Z - the same, after removing the applied effort.
Расположение элемента корпуса 1 сервомотора позвол ет применить прелагаемый способ 1.ФИГ.1). Элемент копуса содержит сборочную обечайку 2 дл последующего введени в другой подобный элемент корпуса, плоское кольцевое основание 3 и оболочку 4 переменного профил , соедин ющую обчайку 2 с плоским основанием 3. Окочательный профиль оболочки 4 в существенной степени параболический. Кольцева деталь 5 жесткости опираетс на внутреннюю поверхность 6 основани 3 и, чтобы избежать деформации последнего, закреплена фиксирующими , винтами 7.The arrangement of the element of the servo motor body 1 permits the proposed method 1. FIG. 1). The copus element contains an assembly shell 2 for subsequent insertion into another similar body element, a flat annular base 3 and a sheath 4 of a variable profile connecting the tap 2 with a flat base 3. The final profile of the sheath 4 is essentially parabolic. The annular stiffening part 5 rests on the inner surface 6 of the base 3 and, in order to avoid deformation of the latter, is secured with locking screws 7.
Обечайка 2 опираетс на кольцеву станину 8, а к детали 5 жесткости, помещенной на внутреннюю поверхность 6, прилагаетс усилие определенной величины, направленное перпедикул рно поверхности бив направлении наружу от элемента корпуса 1. Приложение усили происходит в на- правлении стрелки А (фиг.1) и с помощью толкател 9 в форме диска с выемкой в центральной части одной из его сторон дл взаимодействи с периферийной частью детали 5 хсестко ти.The shell 2 rests on the ring base 8, and a stiffness piece 5 placed on the inner surface 6 is subjected to a force of a certain magnitude, directed perpendicularly to the surface of the beam, facing outward from the housing element 1. The force is applied in the direction of arrow A (Fig. ) and using a pusher 9 in the form of a disk with a notch in the central part of one of its sides for interacting with the peripheral part of the part 5 of the nationality.
Приложение указанного усили обепечивает хорошее взаимодействие между контактирующими част ми детали 5 жесткости и основани 3. Оно может привести к посто нной деформации элмента корпуса в осевом направлении на несколько дес тых миллиметра, но деформаци , про вл юща с на этой стадии изготовлени корпуса, позвол ет гарантировать впоследствии абсолютно упругий прогиб корпуса во врем торможени , что соответствует дествующим сейчас fiopMaM. Кроме того, обечайка 2 элемом та корпуса опирает с на станину 8 с по -тощью ее загнутго кра Ю, 1 спользуег.ого дл последующей сборки двух дополнительных элементов корпусгт.,. Следовательно,The application of this force ensures a good interaction between the contacting parts of the stiffness part 5 and the base 3. It can lead to permanent deformation of the housing element in the axial direction by a few tenths of a millimeter, but the deformation that occurs at this stage of the housing production allows ensure subsequently an absolutely elastic hull deflection during deceleration, which corresponds to fiopMaM now in force. In addition, the shell 2 elements of the body rests on the frame 8 with its curved edge U, 1 using it for the subsequent assembly of two additional elements of the housing. Consequently,
00
5five
00
5five
5 U 5 U
5 0 5 5 0 5
00
применение предлагаемого способа очень просто, так как используетс уже существующа особенность конструкции корпуса дл его позиционировани .The application of the proposed method is very simple, since an already existing feature of the hull structure for its positioning is used.
Станина 8 (фи1 .2 и 3) дополнена выступом 11 с заранее определенным положением (т.е. поверхность находитс на определенном рассто нии d от зоны опоры, определенной станиной 8 , на который основание 3 может опиратьс под действием усили , воздействующего на деталь 5 жесткости в тех же услови х, т.е. посредством толкател 9. Величина усили менее критична, чем в способе (фиг.1), однако она должн а быть достаточной дл того, чтобы осуществить эффективный контакт основани 3 с выступом 11. Этот вариант предпочтителен в той мере, что элемент корпуса I может быть заранее грубо отформован на прессе с размерами , превьшающими конечные требуемые его размеры, до применени предлагаемого способа, что позвол ет придать оболочке форму и окончательные размеры с помощью операций,, состо щей в приведении основани 3 в контакт с выступом 1I. Б этих услови х конечный осевой размер элемента корпуса 1 после исчезновени усили (фиг.З рассто ние : ) лучше контролируетс в процессе изготовлени .Frame 8 (phi1.2 and 3) is supplemented with a protrusion 11 with a predetermined position (i.e. the surface is at a certain distance d from the support zone defined by the base 8 on which the base 3 can rest under the force applied to the part 5 stiffness in the same conditions, i.e. by means of the pusher 9. The amount of force is less critical than in the method (Fig. 1), however, it must be sufficient to make effective contact of the base 3 with the protrusion 11. This option preferred to the extent that body element I may b It is coarsely molded in advance on a press with dimensions greater than the final dimensions required, prior to the application of the proposed method, which allows the shell to be shaped and final in size by means of operations, consisting in bringing the base 3 into contact with the protrusion 1.I. The final axial size of the housing element 1 after the disappearance of the forces (Fig. 3) distance is better controlled during the manufacturing process.
Изобретение не ограничиваетс двум указанными вариантами способа. В частности, можно устранить толкатель 9 и осуществл ть приложение усили с помощью фиксирующих винтов 7, т.е. либо давлением исключительно на головки винтов, либо раст жением их резьбовых частей. В последнем случае можно обеспечить лучшее взаимодействие между головками винтов и деталью 5 жесткости.The invention is not limited to these two method variations. In particular, the pusher 9 can be eliminated and the force applied with the help of the fixing screws 7, i.e. either by pressure solely on the heads of the screws, or by stretching their threaded parts. In the latter case, it is possible to provide a better interaction between the heads of the screws and the stiffening part 5.
Claims (5)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR8103271A FR2499924A1 (en) | 1981-02-19 | 1981-02-19 | METHOD FOR CONFORMING A SERVOMOTOR MEMBER WITH ITS REINFORCEMENT |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU1326188A3 true SU1326188A3 (en) | 1987-07-23 |
Family
ID=9255386
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU823390752A SU1326188A3 (en) | 1981-02-19 | 1982-02-17 | Method of forming servo motor body member and joining it with rigidity part |
Country Status (18)
| Country | Link |
|---|---|
| US (1) | US4445263A (en) |
| EP (1) | EP0060161B1 (en) |
| JP (1) | JPS57164850A (en) |
| KR (1) | KR880001731B1 (en) |
| AR (1) | AR226142A1 (en) |
| AU (1) | AU542829B2 (en) |
| BR (1) | BR8200853A (en) |
| CA (1) | CA1180172A (en) |
| DE (1) | DE3263216D1 (en) |
| ES (1) | ES8301788A1 (en) |
| FR (1) | FR2499924A1 (en) |
| MX (1) | MX157167A (en) |
| PL (1) | PL129408B1 (en) |
| PT (1) | PT74420B (en) |
| RO (1) | RO82947B (en) |
| SU (1) | SU1326188A3 (en) |
| TR (1) | TR22302A (en) |
| YU (1) | YU45858B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4574455A (en) * | 1984-09-04 | 1986-03-11 | Allied Corporation | Method of manufacturing a shell with an integral reinforcing plate |
| AU571785B2 (en) * | 1985-09-30 | 1988-04-21 | Jidosha Kiki Co. Ltd. | Brake booster |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2244927A (en) * | 1938-03-16 | 1941-06-10 | Thomas J Vanstone | Wheel press |
| US2696240A (en) * | 1949-10-28 | 1954-12-07 | Crowder John Hardin | Dent remover |
| FR2139613B1 (en) * | 1971-05-03 | 1974-04-05 | Dunlop Sa | |
| DE2129547B2 (en) * | 1971-06-10 | 1980-05-29 | Mannesmann Kronprinz Ag, 5650 Solingen | Heavy goods vehicle discs - have flat surfaces to production of by subsequent levelling prior produced serrations |
| US3756063A (en) * | 1972-04-27 | 1973-09-04 | Grotnes Machine Works Inc | Shrink forming apparatus with axial run-out tooling |
| DE2224027A1 (en) * | 1972-05-17 | 1973-11-22 | Ford Werke Ag | PROCEDURE FOR CIRCULAR AND END RUNNING CORRECTION OF SHEET STEEL DISC WHEELS, IN PARTICULAR FOR MOTOR VEHICLES |
| FR2459166A1 (en) * | 1979-06-15 | 1981-01-09 | Dba | BRAKE ASSIST SERVOMOTOR |
| JPS5766062A (en) * | 1980-10-01 | 1982-04-22 | Aisin Seiki Co Ltd | Attaching method for reinforcing plate of brake booster |
-
1981
- 1981-02-19 FR FR8103271A patent/FR2499924A1/en active Granted
-
1982
- 1982-01-27 AU AU79876/82A patent/AU542829B2/en not_active Ceased
- 1982-02-01 KR KR8200404A patent/KR880001731B1/en active
- 1982-02-01 US US06/344,277 patent/US4445263A/en not_active Expired - Lifetime
- 1982-02-04 CA CA000395573A patent/CA1180172A/en not_active Expired
- 1982-02-08 YU YU26382A patent/YU45858B/en unknown
- 1982-02-10 RO RO106591A patent/RO82947B/en unknown
- 1982-02-12 PT PT74420A patent/PT74420B/en not_active IP Right Cessation
- 1982-02-15 MX MX191391A patent/MX157167A/en unknown
- 1982-02-15 EP EP82400261A patent/EP0060161B1/en not_active Expired
- 1982-02-15 DE DE8282400261T patent/DE3263216D1/en not_active Expired
- 1982-02-17 PL PL1982235120A patent/PL129408B1/en unknown
- 1982-02-17 SU SU823390752A patent/SU1326188A3/en active
- 1982-02-17 BR BR8200853A patent/BR8200853A/en not_active IP Right Cessation
- 1982-02-18 TR TR1158A patent/TR22302A/en unknown
- 1982-02-18 AR AR288476A patent/AR226142A1/en active
- 1982-02-18 ES ES509718A patent/ES8301788A1/en not_active Expired
- 1982-02-19 JP JP57024664A patent/JPS57164850A/en active Granted
Non-Patent Citations (1)
| Title |
|---|
| Мещерин В.Т. Листова штамповка. Атлас схем. М.: Машиностроение, с. 826, л. 186. * |
Also Published As
| Publication number | Publication date |
|---|---|
| MX157167A (en) | 1988-10-31 |
| AR226142A1 (en) | 1982-05-31 |
| CA1180172A (en) | 1985-01-02 |
| JPS57164850A (en) | 1982-10-09 |
| EP0060161B1 (en) | 1985-04-24 |
| PL235120A1 (en) | 1982-10-25 |
| ES509718A0 (en) | 1983-01-16 |
| EP0060161A1 (en) | 1982-09-15 |
| FR2499924B1 (en) | 1985-03-08 |
| DE3263216D1 (en) | 1985-05-30 |
| KR830008869A (en) | 1983-12-16 |
| KR880001731B1 (en) | 1988-09-10 |
| US4445263A (en) | 1984-05-01 |
| YU26382A (en) | 1990-04-30 |
| BR8200853A (en) | 1982-12-28 |
| PT74420A (en) | 1982-03-01 |
| FR2499924A1 (en) | 1982-08-20 |
| AU542829B2 (en) | 1985-03-14 |
| TR22302A (en) | 1987-01-15 |
| AU7987682A (en) | 1982-08-26 |
| ES8301788A1 (en) | 1983-01-16 |
| RO82947B (en) | 1984-01-30 |
| YU45858B (en) | 1992-09-07 |
| JPH032702B2 (en) | 1991-01-16 |
| PL129408B1 (en) | 1984-05-31 |
| RO82947A (en) | 1984-01-14 |
| PT74420B (en) | 1983-11-15 |
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